A boundary node method for airfoils based on the Dirichlet condition
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Publication:1841040
DOI10.1016/S0045-7825(00)00182-1zbMath0976.76050MaRDI QIDQ1841040
Publication date: 2 January 2002
Published in: Computer Methods in Applied Mechanics and Engineering (Search for Journal in Brave)
Dirichlet boundary conditionnumerical quadraturesingular kernelsregularizationsnonsingular integral equationJoukowsky airfoilthin airfoilsvan de Vooren airfoil
Boundary element methods applied to problems in fluid mechanics (76M15) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)
Related Items (6)
Global error analysis of two-dimensional panel methods for Dirichlet formulation ⋮ Regularized boundary integral methods for three-dimensional potential flows ⋮ Non-singular boundary integral formulations for plane interior potential problems ⋮ Panel method for mixed configurations with finite thickness and zero thickness ⋮ A regularized boundary integral method in potential theory ⋮ Global error analysis of two-dimensional panel methods for Neumann formulation
Cites Work
- A boundary element approach to the 2D potential flow problem around airfoils with cusped trailing edge
- A direct boundary integral method for the three-dimensional lifting flow
- Non-singular direct formulation of boundary integral equations for potential flows
- Subsonic Potential Aerodynamics for Complex Configurations : A General Theory
- A higher‐order boundary element method for three‐dimensional potential problems
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